Considerations on design parameters for attitude control of spacecraft using port-controlled Hamiltonian systems

Authors

Tomoya Sakamoto, Yuki Akiyama, Mai Bando, Shinji Hokamoto

Abstract

In previous research, a controller design procedure via generalized canonical transformations has been proposed to keep the passivity feature of Port-controlled Hamiltonian systems. The procedure has a general form and is applicable to spacecraft’s attitude motion described with quaternion parameters. This paper investigates the roles of several design parameters in the generalized canonical transformations. Special attention is placed on the relation between the shape of Lyapunov functions and the convergence speed of the state variables. Furthermore, from the analysis utilizing the linearized form of the Port-controlled Hamiltonian system, the guideline to decide the preferable ratio between two parameters in the design procedure is proposed.

Citation

• Journal: 2017 56th Annual Conference of the Society of Instrument and Control Engineers of Japan (SICE)
• Year: 2017
• Volume:
• Issue:
• Pages: 464–469
• Publisher: IEEE
• DOI: 10.23919/sice.2017.8105722

BibTeX

@inproceedings{Sakamoto_2017,
  title={{Considerations on design parameters for attitude control of spacecraft using port-controlled Hamiltonian systems}},
  DOI={10.23919/sice.2017.8105722},
  booktitle={{2017 56th Annual Conference of the Society of Instrument and Control Engineers of Japan (SICE)}},
  publisher={IEEE},
  author={Sakamoto, Tomoya and Akiyama, Yuki and Bando, Mai and Hokamoto, Shinji},
  year={2017},
  pages={464--469}
}

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References

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